As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HFEC INSPECTION OF THE AFFECTED AREA PER SB737-53A1204 REV 2 INSTRUCTIONS THAT IS RELATED WITH AD2018-04-06, IT WAS FOUND AT BS 360 STR 9L LEVEL THE ATTACHMENT CLIP CRACKED. THE AFFECTED CLIP WAS REPLACED IAW ASAP E.O. # 5322-024 REV-IR, SUPPORTED BY FAA FORM 8110-3 AND AMOC APPROVAL TO AD2018-04-06.